An Experimental Investigation of the Effects of Mach Number, Stabilizer Dihedral, and Fin Torsional Stiffness on the Transonic Flutter Charachteristics of a Tee-tail
Title | An Experimental Investigation of the Effects of Mach Number, Stabilizer Dihedral, and Fin Torsional Stiffness on the Transonic Flutter Charachteristics of a Tee-tail PDF eBook |
Author | Norman S. Land |
Publisher | |
Pages | 28 |
Release | 1961 |
Genre | Loads (Mechanics) |
ISBN |
An Experimental Investigation of the Effects of Mach Number, Stabilizer Dihedral, and Fin Torsional Stiffness on the Transonic Flutter Characteristics of a Tee-tail
Title | An Experimental Investigation of the Effects of Mach Number, Stabilizer Dihedral, and Fin Torsional Stiffness on the Transonic Flutter Characteristics of a Tee-tail PDF eBook |
Author | Norman S. Land |
Publisher | |
Pages | 28 |
Release | 1957 |
Genre | Aerodynamics, Transonic |
ISBN |
Monthly Catalog of United States Government Publications
Title | Monthly Catalog of United States Government Publications PDF eBook |
Author | |
Publisher | |
Pages | 1878 |
Release | 1961 |
Genre | Government publications |
ISBN |
Technical Abstract Bulletin
Title | Technical Abstract Bulletin PDF eBook |
Author | Defense Documentation Center (U.S.) |
Publisher | |
Pages | 1116 |
Release | 1961-02 |
Genre | Technology |
ISBN |
An Experimental Investigation of the Effects of Mach Number, Stabilizer Dihedral, and Fin Torsional Stiffness on the Transonic Flutter Characteristics of a Tee-tail
Title | An Experimental Investigation of the Effects of Mach Number, Stabilizer Dihedral, and Fin Torsional Stiffness on the Transonic Flutter Characteristics of a Tee-tail PDF eBook |
Author | Norman S. Land |
Publisher | |
Pages | 1 |
Release | 1961 |
Genre | |
ISBN |
A transonic flutter investigation was made of elastically and dynamically scaled models of the tee-tail of a patrol bomber. It was found that removal of the 15 degrees dihedral of the stabilizer used on the airplane raised the flutter boundary to higher dynamic pressures. The effect of Mach number on the flutter boundary was different for dihedral angles of 0 degrees and 15 degrees. The dynamic pressure at the flutter boundary increased approximately linearly with the torsional stiffness of the fin. Highspeed motion pictures indicated that the flutter mode consisted primarily of fin bending and fin torsion. (Author).
A Collection of Technical Papers on Structures and Materials
Title | A Collection of Technical Papers on Structures and Materials PDF eBook |
Author | |
Publisher | |
Pages | 354 |
Release | 1975 |
Genre | Airplanes |
ISBN |
NASA Technical Note
Title | NASA Technical Note PDF eBook |
Author | |
Publisher | |
Pages | 572 |
Release | 1975 |
Genre | |
ISBN |